Helicopter Vibration Reduction Using Single Crystal And Soft Piezoceramic Shear Induced Active Blade Twist

Helicopter Vibration Reduction Using Single Crystal And Soft Piezoceramic Shear Induced Active Blade Twist

Bibliographic Details
Main Author: Thakkar, Dipali
Other Authors: Ganguli, Ranjan
Language:en_US
Published: 2011
Subjects:
Helicopters - Vibration
Piezoceramics - Shear Dynamics
Rotors (Helicopters)
Helicopter Rotor Blades
Rotor Dynamics
Aeroelastic Analysis
Rotating Beams
Helicopters - Aerodynamics
Helicopter - Aeroelasticity
Rotar Blade
Piezoceramic Actuation
Helicopter Vibration Reduction
Helicopter Rotor
Aeronautics
Online Access:http://etd.iisc.ernet.in/handle/2005/1477
http://etd.ncsi.iisc.ernet.in/abstracts/1897/G19167-Abs.pdf

Internet

http://etd.iisc.ernet.in/handle/2005/1477
http://etd.ncsi.iisc.ernet.in/abstracts/1897/G19167-Abs.pdf

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